Blade Apparatus With Blade Pitch Adjustability

FIELD OF THE DISCLOSURE

The present disclosure relates to adjustability of the pitch of a blade for a work vehicle.

BACKGROUND OF THE DISCLOSURE

There are prior art crawler dozers for use in heavy duty applications which have a base machine and a blade apparatus coupled to the base machine. The blade apparatus has a blade configured to push large quantities of soil, sand, rubble, or other material, earthen or otherwise, and a blade driver configured to interconnect the blade and the base machine.

The blade driver has a frame with a pair of push-beams positioned laterally outward from and pivotally coupled to the base machine. The blade is pivotally coupled to the push-beams. The blade driver also has a pitch link in the form of a turnbuckle pivotally coupled to one of the push-beams and the blade and a tilt link in the form of a hydraulic cylinder pivotally coupled to the other push-beam and the blade. The length of the pitch link is adjustable to: adjust the pitch of the blade, and the length of the tilt link is adjustable to adjust the tilt or roll angle of the blade (i.e., the angle of the blade about a fore-aft axis of the dozer). When the pitch link is lengthened, a corresponding amount of tilt angle adjustability is lost since lengthening of the pitch link causes the rod of the tilt link to extend correspondingly.

One type of prior art blade driver has a link anchor on each of the two push-beams: one link anchor for anchoring a frame end of the pitch link and one link anchor for anchoring a frame end of the tilt link. Each such link anchor includes a plurality of mounting points (three) for the respective link, each mounting point having a pair of holes for receiving a pin coupled to the frame end of that link. The mounting points of the two anchors are arranged in pairs, one from the pitch link anchor and one from the tilt link anchor, such that each pair of mounting points corresponds to a respective pitch of the blade relative to the frame. The frame ends of the pitch and tilt links are thus coupleable to any one of the pairs of mounting points to establish the blade at the pitch corresponding to that pair of mounting points, without causing a loss of tilt angle adjustability. As is known in the prior art, dozer operators have complained about the limitations of the pitch adjustability of such an arrangement due to its coarse pitch resolution.

SUMMARY OF THE DISCLOSURE

According to an aspect of the present disclosure, there is provided a blade apparatus for a work vehicle. The blade apparatus comprises a frame, a blade pivotally coupled to the frame, first and second link anchors, and first and second links. Each of the first and second link anchors is mounted to the blade and comprises a plurality of mounting points. The mounting points of the first and second link anchors are arranged in pairs of mounting points, one from the first link anchor and one from the second link anchor, such that each pair of mounting points corresponds to a respective pitch of the blade relative to the frame.

The first and second links are pivotally coupled to the frame and pivotally coupled respectively to the mounting points of a selected one of the pairs of mounting points to establish the blade at the pitch corresponding to that pair of mounting points. The pitch of the blade can be adjusted by changing to which pair of mounting points the first and second links are pivotally coupled respectively.

Mounting of the link anchors with multiple mounting points to the blade rather than the push-beams provides a number of benefits. It affords ergonomic pitch adjustment in a location less susceptible to accumulation of packed material, without a corresponding loss of tilt angle adjustability. Further, the anchors can be designed to position the mounting points so as to achieve a generally desired pitch resolution between the mounting points, such as a relatively fine pitch resolution as compared to the relatively coarse pitch resolution afforded by the afore-mentioned prior art link anchors mounted to the push-beams. Such frame-mounted link anchors are limited in pitch resolution by stress considerations.

The above and other features will become apparent from the following description and the attached drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

The detailed description of the drawing refers to the accompanying figures in which:

FIG. 1 is left side elevation view showing a work vehicle exemplarily in the form of a crawler dozer having a base machine (shown in simplified form) and a blade apparatus having an adjustable-pitch blade and a blade driver interconnecting the blade and the base machine;

FIG. 2 is a perspective view of the blade apparatus showing a pitch link (foreground) and a tilt link (background) pivotally coupled respectively to first and second push-beams and to selected mounting points of pitch link and tilt link anchors establishing the blade at a corresponding pitch relative to the frame;

FIG. 3 is a perspective view showing a blade end of the pitch link pivotally coupled to a middle mounting point of the pitch link anchor and a frame end of the pitch link pivotally coupled to a link anchor mounted on one of the push-beams;

FIG. 4 is a left side elevation view showing the plurality of mounting points of the pitch link anchor;

FIG. 5 is a sectional view taken along lines 5-5 of FIG. 3;

FIG. 6 is a right side elevation view of the pitch link anchor;

FIG. 7 is a rear elevation view of the blade;

FIG. 8 is a front elevation view of the blade;

FIG. 9 is a perspective view of the blade, with portions broken away;

FIG. 10 is a partially exploded perspective view; and

FIG. 11 is a side elevation view showing a left lift eye plate mounted to a front wall and channel of the blade.

DETAILED DESCRIPTION OF THE DRAWINGS

Referring to FIG. 1, there is shown a work vehicle 10 exemplarily configured as a crawler dozer (e.g., John Deere 850J crawler dozer). A blade apparatus 12 is included in and provided for use with the vehicle 10. In the case of a crawler dozer, the base machine 14 of the dozer includes an operator station 15 and a tracked undercarriage 16. From the operator station 15, a human operator can control the base machine 14 and the blade apparatus 12 attached thereto.

The undercarriage 16 has left and right track assemblies positioned on laterally opposite sides of the base machine 14 for propulsion of the vehicle 10, the left track assembly shown in simplified form at 17. Each track assembly 17 has a rear drive sprocket 17a rotatably coupled to a main frame of the base machine 14 (the teeth of the sprocket 17a may be included in circumferential segments (e.g., five such segments) aligned circumferentially about the sprocket 17a), a front idler 17b, upper and lower rollers 17c rotatably coupled to a track frame 17d of the track assembly 17, and a track 17e shown diagrammatically and trained about the drive sprocket 17a, the idler 17b, and the rollers 17c. The track 17e has a closed-loop chain, having two rows of interconnected links, and ground-engaging shoes mounted to the chain thereabout for engagement with the ground. A track chain tension adjuster is mounted to the track frame 17d and is coupled to the idler 17b, movable a distance fore-and-aft relative to the track frame 17d, to press the idler 17b against the chain to tension the track 17e. The undercarriage 16 may take any suitable form such as a conventional undercarriage.

The blade apparatus 12 includes a blade 18 and a blade driver 20. The blade 18 is configured for moving large quantities of soil, sand, rubble, or other material, earthen or otherwise. The blade driver 20 interconnects the blade 18 and the base machine 14.

Referring to FIG. 2, the blade driver 20 includes a frame 21. The frame 21 has a pair of push-beams 22, a pair of cross-beams 24, and a center joint 26. Laterally outward ends of the cross-beams 24 are fixed respectively to the push-beams 22 through welding, and laterally inward ends of the cross-beams 24 are movably coupled to one another in, for example, a conventional manner using the center joint 26.

Exemplarily, the center joint 26 includes a pin welded to a first plate welded to the end of the first cross-beams 24, a spherical plain bearing (alternatively, a self-aligning ball bushing) receiving the pin such that the pin is movable linearly along its length within the bearing, and a center piece receiving the bearing and bolted to a second plate welded to the end of the second cross-beam 24 (welds are not shown in the drawings, but are to be understood).

The bearing may be retained in place in the center piece using two circlips, one on each side of the bearing. A link 30 pivotally coupled to a middle portion of the rear of the blade 18 and to a corner tang of the second plate interconnects the blade 18 and the cross-beams 24. The center joint 26 is thus configured to allow rotational movement between the cross-beams 24 by virtue of the bearing and movement of the cross-beams 24 toward and away from one another by virtue of the capacity of the pin to move along its length relative to the bearing. It is to be understood that the center joint 26 may be configured in any suitable manner.

The push-beams 22 are pivotally coupled to and positioned laterally outward from the undercarriage 16 in, for example, a conventional manner using a pair of pivot couplings 19. Exemplarily, each pivot coupling 31 may include a clamp 23 and a trunnion 28. The clamp 23 may have a pair of caps 25, with a first of the caps 25 fixed through welding to the rearward end of a push-beam 22, and a half-moon bushing received in the first cap 25. A ball 27 of the trunnion 28 may be received in the clamp 23 between the caps 25 with the half-moon bushing positioned between the ball 27 and the first cap 25. The caps 25 may be bolted together and shimmed as needed to receive the ball 27. A mounting plate 29 of the trunnion 28 may be bolted to the respective track frame (mounting plate bolts are shown in simplified form without threads, threads being understood). It is to be understood that the push-beams 22 may be pivotally coupled to the undercarriage 16 in any suitable manner.

The blade 18 is pivotally coupled to the frame 21 in, for example, a conventional manner using a pair of pivot couplings 31 of the blade driver 20. Exemplarily, each pivot coupling 31 may include a pivot bracket 32 fixed to a forward end of a respective push-beam 22, a clevis bracket 33 welded to an L-shaped mounting plate 34 welded to a lower portion of the rear of the blade 18 near a respective end of the blade 18, and a lubricated pin 35 extending within holes of the brackets 32, 33 and retained in place by a pin retainer 36. A spherical plain bearing may be mounted within the pivot bracket 32 and retained therein using two circlips, one on either side of the bearing, and may receive the pin 35 therethrough. As an alternative to the coupling 31, the pivot coupling may have a ball and a clamp clamping the ball, the clamp including a pair of caps, with a first of the caps fixed through welding to a forward end of a respective push-beam 22, and a half-moon bushing received in the first cap. The ball may be received in the clamp between the caps with the half-moon bushing positioned between the ball and the first cap. The caps may be bolted together (e.g., using four bolts—two on top and two bottom) and shimmed as needed. The ball may have opposite end portions received in and welded to the holes of two ears of a clevis bracket mounted to the rear of the blade 18. It is to be understood that the blade 18 may be pivotally coupled to the frame 21 in any suitable manner.

A pair of trunnion-mounted hydraulic lift cylinders 37, one of which is shown in FIG. 1, is pivotally coupled to the base machine 14 and to the blade 18 using pivot couplings in, for example, a conventional manner or any other suitable manner. Exemplarily, the cylinders 37 are mounted to either side of the base machine 14 and to the rear of the blade 18 using respective pivot couplings. The operator can raise and lower the blade 18 relative to the base machine 14 using the lift cylinders 32.

The blade apparatus 12 further includes a first or pitch link 38 and a second or tilt link 39, each having an adjustable length. Each link 38, 39 is pivotally coupled to a respective push-beam 22 and to an upper portion of the rear of the blade 18 next to an end of the blade 18. The pitch link 38 is, for example, a turnbuckle having externally threaded opposite ends and an internally threaded sleeve threaded thereto (the external threads of the turnbuckle ends shown diagrammatically and having a thread specification of, for example, M60×3, where the “60” and the “3” represent the major diameter and pitch, respectively, both in millimeters). The external threads of the turnbuckle ends may illustratively be partially exposed outside the turnbuckle sleeve, or, in other embodiments, may be completely hidden within the sleeve to minimize exposure to debris. Alternatively, the pitch link 38 may be a fixed-length link. The tilt link 39 is, for example, a hydraulic cylinder (the extend hose and the retract hose are not shown). As such, the length of the pitch link 38 can be adjusted mechanically to change the pitch of the blade 18 relative to the frame 22, and the length of the tilt link 39 can be adjusted hydraulically, such as by the operator from the operator station 15, to change the tilt angle of the blade 18 relative to a central fore-aft axis 80 of the vehicle 10.

Each link 38, 39 is pivotally coupled to a respective push-beam 22 in, for example, a conventional manner using a link anchor 70. Exemplarily, each link anchor 70 may be mounted on the respective push-beam 22 and may provide a single mounting point for the frame end 40 of the respective link 38, 39. Each link anchor 70 may include a clevis bracket 72, welded to a mounting plate 74 welded to the top of the push-beam 22 and a lubricated pin 76. The pin 76 extends within a pair of holes of the bracket 72 and through a hole of the frame end 40 of the respective link 38, 39 and a bushing positioned on either side of that link 38, 39 and is retained in place by a pin retainer 78. It is to be understood that the links 38, 39 may be pivotally coupled to a respective push-beam 22 in any suitable manner.

The pitch and tilt links 38, 39 are pivotally coupled respectively to a first or pitch link anchor 42 and a second or tilt link anchor 43. The anchors 42, 43 are mounted to the upper portion of the rear of the blade 18 next to the ends of the blade 18.

Each anchor 42,43 has a plurality of mounting points 44, such as three mounting points 44-1, 44-2, and 44-3. The mounting points 44 of the anchors 42, 43 are arranged in pairs of mounting points, one from the pitch link anchor 42 and one from the tilt link anchor 43, such that each pair of mounting points corresponds to a respective pitch of the blade 18 relative to the frame 21.

As such, the frame ends 40 of the pitch and tilt links 38, 39 are pivotally coupled to the frame 21 and the blade ends 41 of the pitch and tilt links 38, 39 are pivotally coupled respectively to the mounting points of a selected one of the pairs of mounting points 44-1, 44-2, or 44-3 to establish the blade 18 at the pitch corresponding to that pair of mounting points 44-1, 44-2, or 44-3. The pitch of the blade 18 can be adjusted by changing to which pair of mounting points 44-1, 44-2, or 44-3 the links 38, 39 are pivotally coupled respectively.

The top, middle, and bottom pairs of mounting points 44-1, 44-2, 44-3 are thus used to establish different pitches of the blade 18. For example, the top, middle, and bottom pairs of mounting points 44-1, 44-2, 44-3 provide a pitch of 53°, 55.3°, and 58° for the blade 18 (pitch shown as angle θ in FIG. 1), this measure of pitch illustrated between the cutting edge of the blade and a horizontal surface (e.g., the ground). As alluded to above, the pitch link 38 may have a fixed length or may have an adjustable length (as with a turnbuckle). Length adjustability of the pitch link 38 may be useful to compensate for manufacturing tolerance stack-up (e.g., variation in cylinder stroke and close lengths in the case of a cylinder for tilt cylinder 39) so as to fine-tune the system, and may be useful to provide even more fine pitch adjustment of the blade 18.

Mounting of the link anchors 42, 43 with multiple mounting points to the blade 18 rather than the push-beams 22 provides a number of benefits. It affords ergonomic pitch adjustment of the blade 18 in a location less susceptible to accumulation of packed material, without a corresponding loss of tilt angle adjustability.

Further, the anchors 42, 43 can be designed to achieve a generally desired pitch resolution between the mounting points 44-1, 44-2, 43, such pitch resolution limited by suitable spacing between the mounting points 44-1, 44-2, 44-3 for stress management of the anchor. For example, the anchors 42, 43 may be designed to provide a relatively fine pitch resolution (e.g., about 2.5° between adjacent pitch positions), as compared to the relatively coarse pitch resolution (e.g., about 5° between adjacent pitch positions) afforded by the afore-mentioned prior art link anchors mounted to the frame push-beams.

Such frame-mounted link anchors are limited in pitch resolution by stress considerations. More particularly, stress considerations limit their height, causing the mounting points to be arranged relative to one another more horizontally than vertically resulting in a more coarse pitch resolution, in contrast to the mounting points 44 of the link anchors 42, 43 which are arranged relative to one another more vertically than horizontally affording a more fine pitch resolution.

Since the anchors 42, 43 are mounted to the blade 18 rather than the push-beams 22, a designer has more design flexibility with respect to the pitch resolution built into the system 12. As mentioned above, the anchors 42, 43 can be designed to have a relatively fine pitch resolution. It is to be appreciated that in other examples the designer could, if desired, provide the anchors 42, 43 with a more coarse pitch resolution.

The pitch resolution is affected by the positioning of the mounting points 44 relative to the link anchors 70 and the blade 18. For sake of description, the link anchor 70 to which the pitch link 42 is coupled may be referred to as the third link anchor 70, and the link anchor 70 to which the tilt link 43 is coupled may be referred to as the fourth link anchor 70. As such, the mounting points 44 of the link anchor 42 are non-equidistant from the third link anchor 70, and the mounting points 44 of the link anchor 43 are non-equidistant from the fourth link anchor 70. The top mounting points 44-1 are positioned farther away from third and fourth link anchors 70, respectively, than the middle mounting points 44-2 such that the pitch angle corresponding to the top mounting points 44-1 is greater than the pitch angle corresponding to the middle mounting points 44-2, and the middle mounting points 44-2 are positioned farther away from the third and fourth link anchors 70, respectively, than the lower mounting points 44-3 such that the pitch angle corresponding to the middle mounting points 44-2 is greater than the pitch angle corresponding to the bottom mounting points 44-3.

The mounting points 44 of each anchor 42, 43 are also non-equidistant from the blade 18. The top mounting points 44-1 are positioned farther away from the blade 18 than the middle mounting points 44-2, and the middle mounting points 44-2 are positioned farther away from the blade 18 than the bottom mounting points 44-3. The positioning of the mounting points 44 relative to the respective link anchor 70 and the blade 18 thus affects the pitch resolution between the mounting points.

Referring to FIGS. 3-5, each of the anchors 42, 43 includes a clevis bracket 47 and a pin 56. The clevis bracket 47 has a first ear 48 and a second ear 48. The ears 48 are mounted to the rear of the blade 18 via an L-shaped mounting plate 58. Each mounting point 44 of each anchor 42, 43 has a pair of holes 54 (see FIG. 5). The first and second ears 48 of each clevis bracket 47 include respectively the first and second holes 54 of each mounting point 44 of that anchor 42, 43.

The holes 54 of each mounting point 44 are configured to receive the pin 56 about which the blade end 41 of the respective link 38, 39 can pivot. To establish a particular pitch for the blade 18, the pin 56 at each anchor 42, 43 is inserted into the holes 54 of the respective mounting point 44-1, 44-2, or 44-3 and fastened in place to the clevis bracket 47. To change the pitch of the blade 18, the pin at each anchor 42, 43 is unfastened and removed from the holes 54 of the current mounting point and inserted into the holes 54 of the new mounting point and re-fastened in place.

Referring to FIG. 5, each ear 48 has a main side plate 48a and a second plate 48b welded to a face of the side plate 48a. The plates 48a, 48b cooperate to provide the holes 54 of the ear 48. The side plates 48a are welded to the mounting plate 58 so as to extend rearwardly therefrom, the mounting plate 58 being welded to the rear of the blade 18, in particular to generally C-shaped top and middle channels 59-1, 59-2 and a flat upper rear plate 61 extending therebetween and welded thereto The mounting plate 58 may have a weld groove formed in a laterally outward edge of the plate 58 to receive a weld therein to facilitate welding together of the plate 58, the side plate 48a of the laterally outward ear 48, the channels 59-1, 59-2, and the plate 61. The rear of the blade 18 further includes a generally C-shaped bottom channel 59-3 and flat lower rear plate 61 extending between and welded to the channels 59-2 and 59-3. The mounting plate 34 is welded to the channels 59-2, 59-3 and the lower rear plate 61.

A gusset 60 reinforces the clevis bracket 47 of each anchor 42, 43 laterally inward thereof. The gusset 60 is welded to the side plate 48a of the laterally inward ear 48 of the anchor 42, 43 and to the mounting plate 58.

The blade end 41 of each link 38, 39 is received between the ears 48 of the respective anchor 42, 43. A bushing 62, one of which is shown, is positioned on either side of the blade end 41 between the blade end 41 and an ear 48 to limit play between the ears 48. The pin 56 extends in the holes 54 through the bushings 62 and the blade end 41.

Referring to FIGS. 5 and 6, a pin retainer 64 retains the pin 56 in place in the holes 54 of the selected mounting point 44. The pin retainer 64 includes a retainer plate 64a and a fastener 64b securing the plate 64a to the side plate 48a of the laterally inward ear 48. The plate 64a is received in an annular groove formed, in the pin 56. The fastener 64b is threaded selectively into one of two threaded retainer holes 65 (threads not shown) formed in the laterally inward ear 48. Exemplarily, each hole 65 may be a through-hole in just the side plate 48a of that ear 48 or a through-hole through both the side plate 48a and plate 48b of that ear 48. The fastener 64a is screwed into the top retainer hole 65 to secure the pin 56 in the holes 54 of the middle mounting point 44-2 (FIG. 5), and is screwed into the bottom retainer hole 65 to secure the pin 56 in the holes 54 of either the top or bottom mounting points 44-1, 44-3 (FIG. 6).

Referring back to FIG. 5, each anchor 42, 43 further includes a cap 66 fixed to the tops of the ears 48 so as to interconnect the tops of those ears 48. Exemplarily, the cap 66 includes a bent, generally rectangular first cap plate 66a and a bent, generally triangular second cap plate 66b. The first cap plate 66a is welded to the tops of the side plates 48a. The second cap plate 66b is positioned between the first cap plate 66a and the blade 18 and is welded to the tops of the side plates 48a, the top of the blade 18, and the first cap plate 66a. A weld groove is formed in an edge of the second cap plate 66b for welding the first and second cap plates 66a, 66b to one another. Alternatively, the cap 66 may be a one-piece structure.

Referring to FIGS. 2 and 7, the blade 18 has a first or left end 110, a second or right end 112, a first or left blade lift eye 114, and a second or right blade lift eye 116. The left and right ends 110, 112 are longitudinally opposite to one another. A hoist can be coupled to each of the left and right blade lift eyes 114, 116 to lift the blade 18.

The left blade lift eye 114 is positioned closer to the left end 110 than the right end 112 atop the blade 18, and the right blade lift eye 116 is positioned closer to the right end 112 than the left end 110 atop the blade 18. The left blade lift eye 114 is inboard of the left end 110, and the right blade lift eye 116 is inboard of the right end 112. Each blade lift eye 114, 116 is thus positioned in a relatively damage-free area such that the blade lift eye 114, 116 is less susceptible to damage than if it were at the respective damage-prone end 110, 112 of the blade 18. Further, the left and right ends 110, 112 of the blade 18 are lower than the left and right blade lift eyes 114, 116, respectively, enhancing operator visibility over the blade ends 110, 112 from the operator's station 15. In addition, although the blade 18 is not configured specifically for mounting of blade control towers near its ends (i.e., it does not include a bolting pattern for mounting of the towers), it is understood that, if so desired, a blade could be configured to have appropriate tower mounts for mounting a blade control tower near each end 110, 112, outboard of the lift eyes 114, 116, such that an inverted Y-shaped hoist may be coupled to the lift eyes 114, 116 without requiring prior removal of the towers from such blade.

The left blade lift eye 114 is included in a first or left lift eye plate 122 of the blade 18, and the right blade lift eye 116 is included in a second or right lift eye plate 124. The left blade lift eye plate 122 is spaced apart from and inboard of a left end-cap plate 118 positioned at the left end 110. The left lift eye plate 122 is inboard of the pitch link anchor 42, the left gusset 60 reinforcing the pitch link anchor 42, and the mounting plate 58 mounted to the rear of the blade 18 and to which the pitch link anchor 42 and the left gusset 60 are mounted. The right lift eye plate 124 is spaced apart from and inboard of a right end-cap plate 120 positioned at the right end 112. The right lift eye plate 124 is inboard of the tilt link anchor 43, the right gusset 60 reinforcing the tilt link anchor 43, and the mounting plate 58 mounted to the rear of the blade 18 and to which the tilt link anchor 43 and the right gusset 60 are mounted.

Referring to FIG. 8, the blade 18 includes a working, front wall 126 configured to perform the work of the blade 18. The front wall 126 includes a main work plate 128, two side work plates 130 flanking the main work plate 128 and welded thereto, a central cutting edge 132 bolted to a bottom portion of the main work plate 128, and two side cutting edges 134 bolted to respective bottom portions of the side plates 130.

Referring to FIG. 9, the channels 59-1, 59-2, 59-3 are welded to the rear of the main work plate 128. To interconnect the channels 59-1, 59-2, 59-3 and the side plates 130 so as to reinforce the side plates 130, at each end region of the channels 59-1, 59-2, 59-3, gussets 136 are welded to the top and bottom walls 137, 139 of the channels 59-1, 59-2, 59-3. A pair of gussets 138 is located within the channel 59-1 at the end regions thereof for internal reinforcement of that channel 59-1.

The end-cap plates 118, 120 are fixed respectively at the ends 110, 112 of the blade 18, as shown, for example, with respect to the left end-cap plate 118 in FIG. 2. The end-cap plates 118, 120 are welded respectively to the ends of the channels 59-1, 59-2, 59-3, the ends of the plates 61, the gussets 136, and the side plates 130. The end-cap plates 118, 120 thus cover respectively the ends of the channels 59-1, 59-2, 59-3. Each end 110, 112 may further include plates 140, 142 welded to the respective end-cap plate 118, 120, strengthening the respective end 110, 112 and providing some wear resistance, as shown, for example, with respect to the left end 110 in FIG. 2.

Referring back to FIG. 7, rearward of the front wall 126, an upper region of the blade 18 includes a central reinforcement structure 144 positioned between the left and right blade lift eye plates 122, 124, a left reinforcement structure 146 positioned between the left end-cap plate 118 and the left blade lift eye plate 114, and a right reinforcement structure 148 positioned between the right end-cap plate 120 and the right blade lift eye plate 116. The central and left reinforcement structures 144, 146 are welded or otherwise coupled to opposite sides of the left blade lift eye plate 122, and the central and right reinforcement structures 144, 148 are welded or otherwise coupled to opposite sides of the right blade lift eye plate 124.

The central reinforcement structure 144 includes a central plate 150 and an angle bar 152. The central plate 150 is welded to the rear of the main work plate 128 and a top wall 137 of the top channel 59-1. The angle bar 152 is welded to the central plate 150 and a rear wall 154 of the top channel 59-1. A pair of inverted V-shaped debris guards 156 may be mounted to the central plate 150 for diverting debris that may flow over the top of the blade 18 away from the lift cylinders 37.

Referring to FIGS. 7 and 10, each of the left and right reinforcement structures 146, 148 includes a base plate 158, a generally triangular laterally outward plate 160, a generally trapezoidal laterally inward plate 162, and a generally triangular laterally intermediate plate 164 laterally between the laterally outward plate 160 and the laterally inward plate 162. The base plate 158 is welded to the respective end-cap plate 118, 120, the main work plate 128, the respective side work plate 130, and a top edge of the respective mounting plate 58. The intermediate plate 164 is mounted on edge to the base plate 158 so as to be upright and is welded to the base plate 158, a rear of the main work plate 128, and a laterally inward edge of the respective side work plate 130. The outward plate 160 leans against and is welded to a rear of the respective side work plate 130 and the intermediate plate 164. The inward plate 162 leans against and is welded to a rear of the main work plate 128 and is positioned between and welded to the intermediate plate 164 and the respective blade lift eye plate 122, 124. The illustrated notches formed in the bottom edges of the plates 160, 162 and in the top wall 137 of the top channel 59-1 are provided for manufacturing purposes, to help identify which direction the component is to be oriented.

Referring to FIG. 11, as shown, for example, with respect to the left blade lift plate 122, each of the left and right blade lift eye plates 122, 124 includes a body 166 and a tail 168 depending from the body 166 behind the rear wall 154 of the top channel 59-1, the body 166 and the tail 168 cooperating such that the respective plate 122, 124 is a one-piece construction. The body 166 of the left blade lift eye plate 122 includes the left blade lift eye 114, and the body 166 of the right blade lift eye plate 124 includes the right blade lift eye 116.

Each of the left and right blade lift eye plates 122, 124 is mounted on edge to the top channel 59-1 and the front wall 126. A front peripheral edge 170 of the body 166 is welded or otherwise mounted to the rear of the main work plate 128. A bottom peripheral edge 172 of the body 166 is welded or otherwise mounted to a top wall 137 of the top channel 59-1. A front peripheral edge 174 of the tail 168 is welded or otherwise mounted to a rear wall 154 of the top channel 59-1. The body 166 is welded to the rear of the main work plate 128, the top wall 137 of the top channel 59-1, the respective inward plate 162, the central plate 150, and the angle bar 152 such that the body 166 is positioned laterally between the respective inward plate 162 and the central plate 150 and laterally between the respective inward plate 162 and the angle bar 152. The tail 168 is welded to the rear wall 154 of the top channel 59-1, the respective mounting plate 58, and the angle bar 152 such that the tail 168 is positioned laterally between the respective mounting plate 58 and the angle bar 152.

It is to be understood that, for purposes of the pitch and tilt link anchors 42, 43, the blade lift eyes 114, 116 may be positioned at the ends or inboard of the ends 110, 112. It is to be understood that, for purposes of the blade lift eyes 114, 116, the pitch and tilt link anchors 42, 43 may have any number of mounting points (e.g., one, two, three, or more).

The blade apparatus 12 may be made:of conventional or other suitable materials. Exemplarily, the cutting edges 132, 134 may be made of hardened, wear-resistant steel. Further exemplarily, the structural components of the blade 18 and blade driver 20, as well as other components welded to the blade or blade driver 20 (e.g., ears 48, caps 66, mounting plates 58, gussets 60), may be made of high-strength, low alloy steel (e.g., plates 128, 130 having 100,000 psi yield strength and remainder having 50,000 psi yield strength).

While the disclosure has been illustrated and described in detail in the drawings and foregoing description, such illustration and description is to be considered as exemplary and not restrictive in character, it being understood that illustrative embodiments have been shown and described and that all changes and modifications that come within the spirit of the disclosure are desired to be protected. It will be noted that alternative embodiments of the present disclosure may not include all of the features described yet still benefit from at least some of the advantages of such features. Those of ordinary skill in the art may readily devise their own implementations that incorporate one or more of the features of the present disclosure and fall within the spirit and scope of the present invention as defined by the appended claims.

Blade Apparatus With Blade Pitch Adjustability

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CPC

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Abstract

Description

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